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<H2>AIRFOILS INDEX</H2>
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<tr valign="top"><td width="25%" align="left"><b>Airfoils available:</b></td>
                 <td width="75%" align="left">

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<tr> <td> <b>NACA Wing Sections</b> - Re=3.0x10^6 (Measurements by Abbott and von Doenhoff) </td></tr>
<tr> <td> - <A HREF="./../NACA-WS/NACA-63-215/pref.htm"> NACA 63<font
                                               size=2>(2)</font>-215</A>,
            <A HREF="./../NACA-WS/NACA-63-218/pref.htm"> NACA 63<font
                                               size=2>(3)</font>-218</A>,
            <A HREF="./../NACA-WS/NACA-63-221/pref.htm"> NACA 63<font
                                               size=2>(4)</font>-221</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS/NACA-63-415/pref.htm"> NACA 63<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS/NACA-63-418/pref.htm"> NACA 63<font
                                               size=2>(3)</font>-418</A>,
            <A HREF="./../NACA-WS/NACA-63-421/pref.htm"> NACA 63<font
                                               size=2>(4)</font>-421</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS/NACA-64-415/pref.htm"> NACA 64<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS/NACA-64-421/pref.htm"> NACA 64<font
                                               size=2>(4)</font>-421</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS/NACA-65-415/pref.htm"> NACA 65<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS/NACA-65-421/pref.htm"> NACA 65<font
                                               size=2>(4)</font>-421</A>
</td></tr>


<tr> <td> &nbsp; </td></tr>


<tr> <td> <b>NACA Wing Sections</b> - Re=6.0x10^6 (Measurements by Abbott and von Doenhoff) </td></tr>
<tr> <td> - <A HREF="./../NACA-WS-Re6x10e6/NACA-63-215/pref.htm"> NACA 63<font
                                               size=2>(2)</font>-215</A>,
            <A HREF="./../NACA-WS-Re6x10e6/NACA-63-218/pref.htm"> NACA 63<font
                                               size=2>(3)</font>-218</A>,
            <A HREF="./../NACA-WS-Re6x10e6/NACA-63-221/pref.htm"> NACA 63<font
                                               size=2>(4)</font>-221</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS-Re6x10e6/NACA-63-415/pref.htm"> NACA 63<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS-Re6x10e6/NACA-63-418/pref.htm"> NACA 63<font
                                               size=2>(3)</font>-418</A>,
            <A HREF="./../NACA-WS-Re6x10e6/NACA-63-421/pref.htm"> NACA 63<font
                                               size=2>(4)</font>-421</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS-Re6x10e6/NACA-64-415/pref.htm"> NACA 64<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS-Re6x10e6/NACA-64-421/pref.htm"> NACA 64<font
                                               size=2>(4)</font>-421</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS-Re6x10e6/NACA-65-415/pref.htm"> NACA 65<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS-Re6x10e6/NACA-65-421/pref.htm"> NACA 65<font
                                               size=2>(4)</font>-421</A>
</td></tr>


<tr> <td> &nbsp; </td></tr>


<tr> <td> <b>NACA Wing Sections</b> - Re=9.0x10^6 (Measurements by Abbott and von Doenhoff) </td></tr>
<tr> <td> - <A HREF="./../NACA-WS-Re9x10e6/NACA-63-215/pref.htm"> NACA 63<font
                                               size=2>(2)</font>-215</A>,
            <A HREF="./../NACA-WS-Re9x10e6/NACA-63-218/pref.htm"> NACA 63<font
                                               size=2>(3)</font>-218</A>,
            <A HREF="./../NACA-WS-Re9x10e6/NACA-63-221/pref.htm"> NACA 63<font
                                               size=2>(4)</font>-221</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS-Re9x10e6/NACA-63-415/pref.htm"> NACA 63<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS-Re9x10e6/NACA-63-418/pref.htm"> NACA 63<font
                                               size=2>(3)</font>-418</A>,
            <A HREF="./../NACA-WS-Re9x10e6/NACA-63-421/pref.htm"> NACA 63<font
                                               size=2>(4)</font>-421</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS-Re9x10e6/NACA-64-415/pref.htm"> NACA 64<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS-Re9x10e6/NACA-64-421/pref.htm"> NACA 64<font
                                               size=2>(4)</font>-421</A>
</td></tr>
<tr> <td> - <A HREF="./../NACA-WS-Re9x10e6/NACA-65-415/pref.htm"> NACA 65<font
                                               size=2>(2)</font>-415</A>,
            <A HREF="./../NACA-WS-Re9x10e6/NACA-65-421/pref.htm"> NACA 65<font
                                               size=2>(4)</font>-421</A>
</td></tr>


<tr> <td> &nbsp; </td></tr>


<tr> <td> <b>Other NACA Family Airfoils</b> (Velux measurements) </td></tr>
<tr> <td> - <A HREF="./../NACA-63-215-V/pref.htm"> NACA 63<font
                                               size=2>(2)</font>-215(V)</A> - Re=1.1x10^6
</td></tr>
<tr> <td> - <A HREF="./../NACA-63-415-V/pref.htm"> NACA 63<font
                                               size=2>(2)</font>-415(V)</A> - Re=1.6x10^6
</td></tr>
<tr> <td> - <A HREF="./../NACA-63-430-V/pref.htm"> NACA 63-430(V)</A> - Re=1.5x10^6
</td></tr>


<tr> <td> &nbsp; </td></tr>


<tr> <td> <b>RIS&Oslash;-A1 Family Airfoils</b> - Re=1.6x10^6 (Velux measurements) </td></tr>
<tr> <td> - <A HREF="./../RISO-A1-18/pref.htm"> RIS&Oslash;-A1-18</A> </td></tr>
<tr> <td> - <A HREF="./../RISO-A1-21/pref.htm"> RIS&Oslash;-A1-21</A> </td></tr>
<tr> <td> - <A HREF="./../RISO-A1-24/pref.htm"> RIS&Oslash;-A1-24</A> </td></tr>


<tr> <td> &nbsp; </td></tr>


<tr> <td> <b>FFA Airfoils</b> </td></tr>
<tr> <td> - <A HREF="./../FFA-W3-211/FIXED_TRANSITION/pref.htm"> FFA-W3-211, Fixed Transition</A> - Re=1.8x10^6 (FFA measurements) </td></tr>
<tr> <td> - <A HREF="./../FFA-W3-211/FREE_TRANSITION/pref.htm"> FFA-W3-211, Free Transition</A> - Re=1.8x10^6 (FFA measurements) </td></tr>
<tr> <td> - <A HREF="./../FFA-W3-241/pref.htm"> FFA-W3-241</A> - Re=1.5x10^6 (Velux measurements) </td></tr>
<tr> <td> - <A HREF="./../FFA-W3-301/pref.htm"> FFA-W3-301</A> - Re=1.5x10^6 (Velux measurements) </td></tr>


<tr> <td> &nbsp; </td></tr>


<tr> <td> <b>Delft University Airfoils</b> - Re=1.0x10^6 (Delft University measurements) </td></tr>
<tr> <td> - <A HREF="./../DU91-W2-250/pref.htm"> DU91-W2-250</A> </td></tr>
<tr> <td> - <A HREF="./../DU93-W-210/pref.htm"> DU93-W-210</A> </td></tr>


<tr> <td> &nbsp; </td></tr>


<tr> <td> <b>Various Airfoils</b> </td></tr>
<tr> <td> - <A HREF="./../S809/pref.htm"> S809 Airfoil</A> - Re=1.0x10^6 (Delft University measurements) </td></tr>
<tr> <td> - <A HREF="./../S814/pref.htm"> S814 Airfoil</A> - Re=1.0x10^6 (Delft University measurements) </td></tr>

<tr> <td> - <A HREF="./../FX66-S196-V1/pref.htm"> FX66-S196-V1</A> - Re=1.5x10^6 (Measured at Stuttgart University) </td></tr>

<tr> <td> - <A HREF="./../A-AIRFOIL/pref.htm"> A-Airfoil</A> - Re=2.1x10^6 (ONERA measurements) </td></tr>


<tr> <td> &nbsp; </td></tr>


<tr> <td> <b>NASA Airfoils</b> - Re=1.5x10^6 (Measured at Stuttgart University) </td></tr>
<tr> <td> - <A HREF="./../LS1-0413/pref.htm"> LS1-0413</A> </td></tr>
<tr> <td> - <A HREF="./../LS1-0417/pref.htm"> LS1-0417</A> </td></tr>

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